Helicopter control design using feedback linearization techniques

E. Liceaga-Castro; R. Bradley; R. Castro-Linares

Helicopter control design using feedback linearization techniques

E. Liceaga-Castro, R. Bradley, R. Castro-Linares

Producción científica: Contribución a una revista › Artículo de la conferencia › revisión exhaustiva

Resumen

Linear equivalence of nonlinear systems is applied to a helicopter model. The nonlinear control design obtained allows a transformation of the nonlinear helicopter model to a set of four linear controllable and single-input subsystems to be obtained. The main difference between the application presented and other work is that the authors express the diffeomorphic map of the state-input space in explicit form.

Idioma original	Inglés
Páginas (desde-hasta)	533-534
Número de páginas	2
Publicación	Proceedings of the IEEE Conference on Decision and Control
Volumen	1
Estado	Publicada - 1989
Publicado de forma externa	Sí
Evento	Proceedings of the 28th IEEE Conference on Decision and Control. Part 1 (of 3) - Tampa, FL, USA Duración: 13 dic. 1989 → 15 dic. 1989

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title = "Helicopter control design using feedback linearization techniques",

abstract = "Linear equivalence of nonlinear systems is applied to a helicopter model. The nonlinear control design obtained allows a transformation of the nonlinear helicopter model to a set of four linear controllable and single-input subsystems to be obtained. The main difference between the application presented and other work is that the authors express the diffeomorphic map of the state-input space in explicit form.",

author = "E. Liceaga-Castro and R. Bradley and R. Castro-Linares",

year = "1989",

language = "Ingl{\'e}s",

volume = "1",

pages = "533--534",

journal = "Proceedings of the IEEE Conference on Decision and Control",

issn = "0191-2216",

publisher = "Institute of Electrical and Electronics Engineers Inc.",

note = "Proceedings of the 28th IEEE Conference on Decision and Control. Part 1 (of 3) ; Conference date: 13-12-1989 Through 15-12-1989",

}

TY - JOUR

T1 - Helicopter control design using feedback linearization techniques

AU - Liceaga-Castro, E.

AU - Bradley, R.

AU - Castro-Linares, R.

PY - 1989

Y1 - 1989

N2 - Linear equivalence of nonlinear systems is applied to a helicopter model. The nonlinear control design obtained allows a transformation of the nonlinear helicopter model to a set of four linear controllable and single-input subsystems to be obtained. The main difference between the application presented and other work is that the authors express the diffeomorphic map of the state-input space in explicit form.

AB - Linear equivalence of nonlinear systems is applied to a helicopter model. The nonlinear control design obtained allows a transformation of the nonlinear helicopter model to a set of four linear controllable and single-input subsystems to be obtained. The main difference between the application presented and other work is that the authors express the diffeomorphic map of the state-input space in explicit form.

UR - http://www.scopus.com/inward/record.url?scp=0024934377&partnerID=8YFLogxK

M3 - Artículo de la conferencia

AN - SCOPUS:0024934377

SN - 0191-2216

VL - 1

SP - 533

EP - 534

JO - Proceedings of the IEEE Conference on Decision and Control

JF - Proceedings of the IEEE Conference on Decision and Control

T2 - Proceedings of the 28th IEEE Conference on Decision and Control. Part 1 (of 3)

Y2 - 13 December 1989 through 15 December 1989

ER -

Helicopter control design using feedback linearization techniques

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